Pratt & Whitney PW4158

Service difficulty reports · 689

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'PW4158'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2175301Floor Panel · brokenINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 241LH BROKEN. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175302Floor Panel · delaminatedINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 242ZK DELAMINATED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175303Floor Panel · crackedINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 242AQ CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175304Floor Panel · crackedINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 242RH CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175318Floor Panel · crackedINSPECTION TYPE:10YR, MAIN DECK CARGO FLOOR PANEL 242CF CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175324Skin · chafedINSPECTION TYPE:3C, LT WING OTBD FLAP INBD BULLNOSE AT RIB 1 HAS CHAFE DAMAGE. ACCOMPLISHED REPAIR ON LT WING OTBD FLAP INBD BULLNOSE IAW SRM 57-50-00, PARA 4H, FIG 208.Sep 5, 2012 · N167UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA12175353Floor Panel · delaminatedINSPECTION TYPE:10YR, MAIN DECK CARGO FLOOR PANEL 251GF DELAMINATED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175354Floor Panel · delaminatedINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 242BF DELAMINATED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175363Floorboard · crackedINSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 241RH LOWER SURFACE IS CRACKED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175364Floorboard · crackedINSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 232NJ LOWER SKIN IS CRACKED IN TWO PLACES. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175389Floorboard · brokenINSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 221EG IS BROKEN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175396Floor Panel · crackedINSPECTION TYPE:10YR, MAIN DECK CARGO FLOOR PANEL 242VM CRACKED AND TEFLON SEAL DISBONDED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A. Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175437Floorboard · crackedINSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 231RG IS CRACKED AND DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175438Floorboard · damagedINSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 241SM IS DAMAGED AT FWD INBD CORNER. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.Sep 5, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR FDEA201209043222Floor Support · corrodedAFT HOLD FLOOR SUPPORT BETWEEN FR63 AND FR 64 LT FROM CENTER FOUND CORRODED. REPLACED IAW SRM 51-40-21.Sep 4, 2012 · N718FD · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2175185Floorboard · crackedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 222DG LOWER SKIN IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175187Floorboard · damagedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 222CG HAS CORRODED INSERTS AND LOWER SKIN IS DAMAGED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175188Floorboard · crackedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 221EG HAS LOWER SKIN CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175189Floorboard · damagedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232LT HAS LOWER SKIN EDGE DAMAGE FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175190Floorboard · damagedINSPECTION TYPE:SV, MAIN CABIN FLOORBOARD 231RH HAS EDGE DAMAGE. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175194Floorboard · puncturedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231LG HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175203Floorboard · damagedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231KJ HAS EDGE DAMAGE. FABRICATED MAIN CABIN FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.Sep 4, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175240Floor Panel · crackedINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 231PJ CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175241Floor Panel · crackedINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 231WG CRACKED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175242Floor Panel · crackedINSPECTION TYPE: 10YR MAIN DECK CARGO FLOOR PANEL 231MJ CRACKED. REAPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175243Floor Panel · delaminatedINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 231RH DELAMINATED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175254Floorboard · delaminatedINSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 231TG LOWER SKIN IS DELAMINATED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175255Floorboard · puncturedINSPECTION TYPE: 10YR MAIN CABIN FLOORBOARD 232KG LOWER SKIN IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175256Floorboard · brokenINSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 231NJ HAS MULTIPLE CRACKS, PUNCTURES AND CORNER IS BROKEN. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175390Floor Panel · damagedINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 241GN IS DAMAGED ON AFT EDGE. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552-B, APPENDIX A/B.Sep 4, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175391Floor Panel · damagedINSPECTION TYPE:10YR, MAIN DECK CARGO FLOOR PANEL 241YK IS DAMAGED ON THE CORNER. FABRICATED FLOOR PANEL IAW EO A300-5320-40552-B, APPENDIX A/B.Sep 4, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175423Floorboard · crackedINSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD NR 231QC LOWER SKIN HAS TWO CRACKS. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 4, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR FDEA201209033213Frame · crackedCRACK INDICATION ON FR40 RT WING ROOT REPAIR CARRIED OUT IAW EA6-5315-162966 AND SB A300-57-6052.Sep 3, 2012 · N727FD · Airbus A300B4622R · Fuselage Main, FrameSDR IPXA2175186Floorboard · puncturedINSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232LF LOWER SKIN IS PUNCTURED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 3, 2012 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175236Floorboard · puncturedINSPECTION TYPE: 10YR BULK CARGO FLOORBOARD 161LF HAS A PUNCTURE AT UPPER SKIN. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.Sep 3, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175237Floorboard · damagedINSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 252UJ IS BROKEN. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.Sep 3, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175282Floorboard · delaminatedINSPECTION TYPE: 10YR, BULK CARGO FLOORBOARD 162MF IS DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.Sep 3, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175348Floor Panel · delaminatedINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 252TJ DELAMINATED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 3, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175554Seat Track · corrodedINSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK IS CORRODED AT FR 62 STA -Y953. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.Sep 3, 2012 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2175238Floor Panel · brokenINSPECTION TYPE:10YR, MAIN DECK CARGO FLOOR PANEL 261GH IS BROKEN, DELAMINATED AND DENTED. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-40552-B, APPENDIX A/B.Sep 1, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175362Floorboard · brokenINSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 262LF IS BROKEN. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 1, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA12175397Floor Panel · delaminatedINSPECTION TYPE: 10YR, MAIN DECK CARGO FLOOR PANEL 261PF DELAMINATED. REPAIRED FLOOR PANEL IAW EO A300-5320-42721-B, PARA 6A.Sep 1, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175422Floorboard · brokenINSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 261DM IS BROKEN. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.Sep 1, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175458Seat Track · corrodedINSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK IS CORRODED AT Y450 BETWEEN FR 73-75. ACCOMPLISHED REPAIR ON SEAT TRACK IAW SRM 53-10-16, FIG 201.Sep 1, 2012 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2175537Floorboard · brokenINSPECTION TYPE: 10YR, MAIN CABIN FLOORBOARD 251XJ IS BROKEN. FABRICATED MAIN CABIN FLOORBOARD EO A300-5320-40552-B, APPENDIX B.Sep 1, 2012 · N147UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2175555Seat Track · corrodedINSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK IS CORRODED AT FR 73-74 STA -Y794.3 R & R SEAT TRACK IAW SRM 53-10-16 FIG 201 AND DWG A53279238.Sep 1, 2012 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2175553Seat Track · corrodedINSPECTION TYPE: 10YR, MAIN CABIN SEAT TRACK AT FR 80 STA Y794.3 IS CORRODED. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.Aug 31, 2012 · N147UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2175121Power Supply · inoperativeINSPECTION TYPE: 3C, EMERGENCY EXIT LIGHT P/B SWITCH INTEGRANULAR LAMO AT CREW DOOR DOES NOT LIGHT WHEN PRESSED. R & R EMERGENCY POWER SUPPLY IAW AMM 33-51-14-04.Aug 29, 2012 · N164UP · Airbus A300F4622R · Emergency LightingSDR IPXA2175056Skin · damagedA HOLE WAS FOUND IN LOWER SKIN OF RT INBD FLAP. 26.5" FROM T/E AND 25.25" INBD OF P PANEL EDGE. REPAIRED IAW EO A300-5750-48318B.Aug 27, 2012 · N134UP · Airbus A300F4622R · Trailing Edge FlapsSDR FDEA201208263169Floorbeam · corrodedCARGO BAY FR 69 FLOORBEAM CORRODED. BLEND OUT THE CORROSION IAW SRM 51-74-10 AND APPLY ALODINE IAW SRM 51-21-10. MEASURE THE REMAINING THICKNESS IAW NTM51-10-04, THE REMAINING THICKNESS IS 0.075 INCHES. ORIGINAL THICKNESS IS 0.098", FOUND OUT OF LIMITS IAWAug 26, 2012 · N741FD · Airbus A300B4622R · Fuselage Main, Floor Beam
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